Proppants and Methods of Making the Same

US2016376199A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016376199-A1
Application numberUS-201414903457-A
CountryUS
Kind codeA1
Filing dateAug 6, 2014
Priority dateAug 7, 2013
Publication dateDec 29, 2016
Grant date

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

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Synthetic ceramic proppants are described. Methods to make these proppants and methods of using these proppants are also described.

First claim

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What is claimed is: 1 . A proppant comprising a porous core and a shell surrounding the core, the shell including a transition region and an outer shell surrounding the transition region, wherein an average transition region density is greater than an average outer shell density and the average shell density is greater than an average core density. 2 . The proppant of claim 1 , wherein the average transition region density is at least 5% greater than the average outer shell density, and/or the average transition region density is at least 5% greater than the average core density. 3 . The proppant of claim 1 , wherein the core is substantially hollow. 4 . The proppant of claim 1 , wherein the core, the transition region, the outer shell, or any combination thereof comprises graphene. 5 . A proppant comprising a porous core, a transition region surrounding the core, and an outer shell surrounding the transition region, wherein an average transition region porosity is less than an average outer shell porosity and the average outer shell porosity is less than an average core porosity. 6 . The proppant of claim 5 , wherein a) the average transition region porosity is less than the average outer shell porosity, or b) the average transition region porosity is less compared to the average core porosity, or both a) and b). 7 . The proppant of claim 5 , wherein the core is substantially hollow and the average core porosity is about 100 vol % based on the total volume of the core. 8 .- 20 . (canceled) 21 . A method of making a sintered ceramic proppant comprising: forming a substantially spherical green body core comprising one or more ceramic particulate materials; forming, at the same time or afterwards, a green body shell around the green body core, wherein the green body shell comprises at least one ceramic particulate material that results in a green core/shell body; sintering the green core/shell body, and, during sintering, diffusing (or otherwise migrating) at least a portion of the green body core into the green body shell to form a sintered ceramic proppant comprising a porous core, a transition region surrounding the core, and an outer shell surrounding the transition region, wherein an average transition region density is greater than an outer average shell density and the average outer shell density is greater than an average core density. 22 . The method of claim 21 , wherein the sintering comprises heating the green/core shell body to at least 500° C. 23 .- 25 . (canceled) 26 . The method of claim 21 , wherein the green body core has a weight ratio of SiO 2 to Al 2 O 3 of 2.3 or higher and a combined weight percentage of Na 2 O and K 2 O of 5.0 or higher based on the total dry weight of the core. 27 . The method of claim 21 , wherein the green body core comprises at least 5.0 wt % of components having a melting point of less than 1200° C. and less than 95 wt % of components having a melting point greater than 1200° C. based on the total dry weight of the core. 28 . The method of claim 21 , wherein the green body core comprises at least 5.0 wt % of components having a melting point of less than 1200° C., less than 7.0% wt % of components having a melting point greater than 1200° C. and less than 1500° C., and less than 88 wt % of components having a melting point greater than 1500° C. based on the total dry weight of the core. 29 . The method of claim 21 , wherein the green body core comprises at least 5.0 wt % of components having a melting point of less than 1200° C., less than 92 wt % of components having a melting point greater than 1200° C. and less than 2100° C., and less than 3.0 wt % of components having a melting point greater than 2100° C. based on the total dry weight of the core. 30 . The method of claim 21 , wherein the green body core comprises one or more fluxing agents and one or more non-fluxing ceramic materials, wherein the melting points of the fluxing agents are less than the melting points than the non-fluxing ceramic materials. 31 . The method of claim 21 , sintered ceramic proppant comprises a substantially hollow core. 32 .- 39 . (canceled) 40 . A proppant comprising a porous core, and a shell surrounding the porous core and comprising a transition region and an outer shell surrounding the transition region, wherein an average transition region density is greater than an average outer shell density, the average outer shell density is greater than an average core density, and the transition region has a glassy phase content of at least 5 vol % based on the total volume of the transition region. 41 . The proppant of claim 40 , wherein the porous core, the transition region, the outer shell, or any combination thereof comprises graphene. 42 .- 85 . (canceled) 86 . A method of forming a conductive ceramic proppant comprising forming a green body comprising graphene, the green body comprising a core, a shell, or both; heating the green body under controlled heating conditions; and sintering the heated green body at an elevated temperature to form a conductive ceramic proppant. 87 . The method of claim 86 , wherein the conductive ceramic proppant is thermally conductive, electrically conductive, or both. 88 .- 90 . (canceled)

Assignees

Inventors

Classifications

  • Carbon · CPC title

  • Shaping around a core which is removed later · CPC title

  • Spheres · CPC title

  • C04B35/52Primary

    based on carbon, e.g. graphite · CPC title

  • Compositions for reinforcing fractures, e.g. compositions of proppants used to keep the fractures open · CPC title

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What does patent US2016376199A1 cover?
Synthetic ceramic proppants are described. Methods to make these proppants and methods of using these proppants are also described.
Who is the assignee on this patent?
Halliburton Energy Services Inc
What technology area does this patent fall under?
Primary CPC classification C04B35/52. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Thu Dec 29 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).